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Thrust and Drag Versus V_e For Straight and Level Flight

by: Kindred Grey

Publication date: 2021-08-04
Usage: Attribution 4.0 International
Topics: Aerodynamics and Aircraft Performance, aircraft performance
Collection: kindredgreyarchive; patron-library-collection
Language: English
Item Size: 226.5K

This image is part of a series that was created for an open textbook, Aerodynamics and Aircraft Performance. The textbook is available here.

Preferred citation:

Kindred Grey (2021). "Thrust and Drag Versus V_e For Straight and Level Flight." CC BY 4.0. Adapted from James F. Marchman (2004). CC BY 4.0.

Alternative text:

A plot is shown with Drag and Thrust in thousand pound increments on the vertical axis, and velocity cap V in increments of 100 feet per second on the horizontal axis. The vertical axis goes from 0 to 7 thousand, while the horizontal axis goes from 0 to 600.